AU600803B2 - Adhesive primer for alumina articles - Google Patents
Adhesive primer for alumina articles Download PDFInfo
- Publication number
- AU600803B2 AU600803B2 AU13058/88A AU1305888A AU600803B2 AU 600803 B2 AU600803 B2 AU 600803B2 AU 13058/88 A AU13058/88 A AU 13058/88A AU 1305888 A AU1305888 A AU 1305888A AU 600803 B2 AU600803 B2 AU 600803B2
- Authority
- AU
- Australia
- Prior art keywords
- alumina
- bracket
- brackets
- silane
- coating
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 title claims abstract description 70
- 239000000853 adhesive Substances 0.000 title abstract description 4
- 230000001070 adhesive effect Effects 0.000 title abstract description 4
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims abstract description 41
- 239000011248 coating agent Substances 0.000 claims abstract description 28
- 238000000576 coating method Methods 0.000 claims abstract description 28
- 239000000377 silicon dioxide Substances 0.000 claims abstract description 20
- 150000003961 organosilicon compounds Chemical class 0.000 claims abstract description 15
- BLRPTPMANUNPDV-UHFFFAOYSA-N Silane Chemical compound [SiH4] BLRPTPMANUNPDV-UHFFFAOYSA-N 0.000 claims abstract description 14
- 229910000077 silane Inorganic materials 0.000 claims abstract description 14
- 239000003522 acrylic cement Substances 0.000 claims abstract description 12
- 238000000034 method Methods 0.000 claims description 39
- XDLMVUHYZWKMMD-UHFFFAOYSA-N 3-trimethoxysilylpropyl 2-methylprop-2-enoate Chemical group CO[Si](OC)(OC)CCCOC(=O)C(C)=C XDLMVUHYZWKMMD-UHFFFAOYSA-N 0.000 claims description 8
- 230000001464 adherent effect Effects 0.000 claims description 6
- 239000006087 Silane Coupling Agent Substances 0.000 claims description 3
- 239000000203 mixture Substances 0.000 claims description 3
- 239000004568 cement Substances 0.000 abstract description 6
- 229910052594 sapphire Inorganic materials 0.000 description 23
- 239000010980 sapphire Substances 0.000 description 23
- 238000010438 heat treatment Methods 0.000 description 19
- 239000013078 crystal Substances 0.000 description 17
- 230000037452 priming Effects 0.000 description 13
- 239000000758 substrate Substances 0.000 description 10
- 238000004140 cleaning Methods 0.000 description 8
- 239000000243 solution Substances 0.000 description 8
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 8
- 238000012360 testing method Methods 0.000 description 7
- 238000003754 machining Methods 0.000 description 6
- 239000008367 deionised water Substances 0.000 description 4
- 229910021641 deionized water Inorganic materials 0.000 description 4
- 230000004907 flux Effects 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 239000000155 melt Substances 0.000 description 4
- 238000005498 polishing Methods 0.000 description 4
- KFZMGEQAYNKOFK-UHFFFAOYSA-N Isopropanol Chemical compound CC(C)O KFZMGEQAYNKOFK-UHFFFAOYSA-N 0.000 description 3
- 239000012298 atmosphere Substances 0.000 description 3
- 238000000151 deposition Methods 0.000 description 3
- 230000008021 deposition Effects 0.000 description 3
- 238000000227 grinding Methods 0.000 description 3
- 238000000197 pyrolysis Methods 0.000 description 3
- 239000002904 solvent Substances 0.000 description 3
- QTBSBXVTEAMEQO-UHFFFAOYSA-N Acetic acid Chemical compound CC(O)=O QTBSBXVTEAMEQO-UHFFFAOYSA-N 0.000 description 2
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- 238000002231 Czochralski process Methods 0.000 description 2
- KRHYYFGTRYWZRS-UHFFFAOYSA-N Fluorane Chemical compound F KRHYYFGTRYWZRS-UHFFFAOYSA-N 0.000 description 2
- PEDCQBHIVMGVHV-UHFFFAOYSA-N Glycerine Chemical compound OCC(O)CO PEDCQBHIVMGVHV-UHFFFAOYSA-N 0.000 description 2
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
- 238000004833 X-ray photoelectron spectroscopy Methods 0.000 description 2
- 238000000137 annealing Methods 0.000 description 2
- OSGAYBCDTDRGGQ-UHFFFAOYSA-L calcium sulfate Chemical compound [Ca+2].[O-]S([O-])(=O)=O OSGAYBCDTDRGGQ-UHFFFAOYSA-L 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 239000003479 dental cement Substances 0.000 description 2
- 239000002274 desiccant Substances 0.000 description 2
- 239000010432 diamond Substances 0.000 description 2
- 229910003460 diamond Inorganic materials 0.000 description 2
- 238000002474 experimental method Methods 0.000 description 2
- 229910052741 iridium Inorganic materials 0.000 description 2
- GKOZUEZYRPOHIO-UHFFFAOYSA-N iridium atom Chemical compound [Ir] GKOZUEZYRPOHIO-UHFFFAOYSA-N 0.000 description 2
- 229910052750 molybdenum Inorganic materials 0.000 description 2
- 239000011733 molybdenum Substances 0.000 description 2
- -1 organosilane compounds Chemical class 0.000 description 2
- 230000001590 oxidative effect Effects 0.000 description 2
- 235000012239 silicon dioxide Nutrition 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- HWSSEYVMGDIFMH-UHFFFAOYSA-N 2-[2-[2-(2-methylprop-2-enoyloxy)ethoxy]ethoxy]ethyl 2-methylprop-2-enoate Chemical compound CC(=C)C(=O)OCCOCCOCCOC(=O)C(C)=C HWSSEYVMGDIFMH-UHFFFAOYSA-N 0.000 description 1
- SJECZPVISLOESU-UHFFFAOYSA-N 3-trimethoxysilylpropan-1-amine Chemical compound CO[Si](OC)(OC)CCCN SJECZPVISLOESU-UHFFFAOYSA-N 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910013184 LiBO Inorganic materials 0.000 description 1
- AMFGWXWBFGVCKG-UHFFFAOYSA-N Panavia opaque Chemical compound C1=CC(OCC(O)COC(=O)C(=C)C)=CC=C1C(C)(C)C1=CC=C(OCC(O)COC(=O)C(C)=C)C=C1 AMFGWXWBFGVCKG-UHFFFAOYSA-N 0.000 description 1
- NBIIXXVUZAFLBC-UHFFFAOYSA-N Phosphoric acid Chemical compound OP(O)(O)=O NBIIXXVUZAFLBC-UHFFFAOYSA-N 0.000 description 1
- 239000004698 Polyethylene Substances 0.000 description 1
- BOTDANWDWHJENH-UHFFFAOYSA-N Tetraethyl orthosilicate Chemical compound CCO[Si](OCC)(OCC)OCC BOTDANWDWHJENH-UHFFFAOYSA-N 0.000 description 1
- NOZAQBYNLKNDRT-UHFFFAOYSA-N [diacetyloxy(ethenyl)silyl] acetate Chemical compound CC(=O)O[Si](OC(C)=O)(OC(C)=O)C=C NOZAQBYNLKNDRT-UHFFFAOYSA-N 0.000 description 1
- 229960000583 acetic acid Drugs 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- NIXOWILDQLNWCW-UHFFFAOYSA-N acrylic acid group Chemical group C(C=C)(=O)O NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- AZDRQVAHHNSJOQ-UHFFFAOYSA-N alumane Chemical group [AlH3] AZDRQVAHHNSJOQ-UHFFFAOYSA-N 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- QUZSUMLPWDHKCJ-UHFFFAOYSA-N bisphenol A dimethacrylate Chemical compound C1=CC(OC(=O)C(=C)C)=CC=C1C(C)(C)C1=CC=C(OC(=O)C(C)=C)C=C1 QUZSUMLPWDHKCJ-UHFFFAOYSA-N 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 239000007822 coupling agent Substances 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- OLLFKUHHDPMQFR-UHFFFAOYSA-N dihydroxy(diphenyl)silane Chemical compound C=1C=CC=CC=1[Si](O)(O)C1=CC=CC=C1 OLLFKUHHDPMQFR-UHFFFAOYSA-N 0.000 description 1
- YYLGKUPAFFKGRQ-UHFFFAOYSA-N dimethyldiethoxysilane Chemical compound CCO[Si](C)(C)OCC YYLGKUPAFFKGRQ-UHFFFAOYSA-N 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 238000005566 electron beam evaporation Methods 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- FWDBOZPQNFPOLF-UHFFFAOYSA-N ethenyl(triethoxy)silane Chemical compound CCO[Si](OCC)(OCC)C=C FWDBOZPQNFPOLF-UHFFFAOYSA-N 0.000 description 1
- WOXXJEVNDJOOLV-UHFFFAOYSA-N ethenyl-tris(2-methoxyethoxy)silane Chemical compound COCCO[Si](OCCOC)(OCCOC)C=C WOXXJEVNDJOOLV-UHFFFAOYSA-N 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 239000012362 glacial acetic acid Substances 0.000 description 1
- 230000007062 hydrolysis Effects 0.000 description 1
- 238000006460 hydrolysis reaction Methods 0.000 description 1
- BFXIKLCIZHOAAZ-UHFFFAOYSA-N methyltrimethoxysilane Chemical compound CO[Si](C)(OC)OC BFXIKLCIZHOAAZ-UHFFFAOYSA-N 0.000 description 1
- PHQOGHDTIVQXHL-UHFFFAOYSA-N n'-(3-trimethoxysilylpropyl)ethane-1,2-diamine Chemical compound CO[Si](OC)(OC)CCCNCCN PHQOGHDTIVQXHL-UHFFFAOYSA-N 0.000 description 1
- 239000003960 organic solvent Substances 0.000 description 1
- 235000011007 phosphoric acid Nutrition 0.000 description 1
- 229920000573 polyethylene Polymers 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 239000010453 quartz Substances 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 150000004760 silicates Chemical class 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 238000004544 sputter deposition Methods 0.000 description 1
- LFQCEHFDDXELDD-UHFFFAOYSA-N tetramethyl orthosilicate Chemical compound CO[Si](OC)(OC)OC LFQCEHFDDXELDD-UHFFFAOYSA-N 0.000 description 1
- FYUZFGQCEXHZQV-UHFFFAOYSA-N triethoxy(hydroxy)silane Chemical compound CCO[Si](O)(OCC)OCC FYUZFGQCEXHZQV-UHFFFAOYSA-N 0.000 description 1
- CPUDPFPXCZDNGI-UHFFFAOYSA-N triethoxy(methyl)silane Chemical compound CCO[Si](C)(OCC)OCC CPUDPFPXCZDNGI-UHFFFAOYSA-N 0.000 description 1
- QQQSFSZALRVCSZ-UHFFFAOYSA-N triethoxysilane Chemical compound CCO[SiH](OCC)OCC QQQSFSZALRVCSZ-UHFFFAOYSA-N 0.000 description 1
- BPSIOYPQMFLKFR-UHFFFAOYSA-N trimethoxy-[3-(oxiran-2-ylmethoxy)propyl]silane Chemical compound CO[Si](OC)(OC)CCCOCC1CO1 BPSIOYPQMFLKFR-UHFFFAOYSA-N 0.000 description 1
- YUYCVXFAYWRXLS-UHFFFAOYSA-N trimethoxysilane Chemical compound CO[SiH](OC)OC YUYCVXFAYWRXLS-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61C—DENTISTRY; APPARATUS OR METHODS FOR ORAL OR DENTAL HYGIENE
- A61C7/00—Orthodontics, i.e. obtaining or maintaining the desired position of teeth, e.g. by straightening, evening, regulating, separating, or by correcting malocclusions
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/009—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone characterised by the material treated
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61C—DENTISTRY; APPARATUS OR METHODS FOR ORAL OR DENTAL HYGIENE
- A61C7/00—Orthodontics, i.e. obtaining or maintaining the desired position of teeth, e.g. by straightening, evening, regulating, separating, or by correcting malocclusions
- A61C7/12—Brackets; Arch wires; Combinations thereof; Accessories therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D7/00—Processes, other than flocking, specially adapted for applying liquids or other fluent materials to particular surfaces or for applying particular liquids or other fluent materials
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/45—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements
- C04B41/50—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements with inorganic materials
- C04B41/5025—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements with inorganic materials with ceramic materials
- C04B41/5035—Silica
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/80—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone of only ceramics
- C04B41/81—Coating or impregnation
- C04B41/85—Coating or impregnation with inorganic materials
- C04B41/87—Ceramics
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Health & Medical Sciences (AREA)
- Materials Engineering (AREA)
- Structural Engineering (AREA)
- Organic Chemistry (AREA)
- Life Sciences & Earth Sciences (AREA)
- Inorganic Chemistry (AREA)
- Public Health (AREA)
- Epidemiology (AREA)
- Dentistry (AREA)
- Animal Behavior & Ethology (AREA)
- General Health & Medical Sciences (AREA)
- Oral & Maxillofacial Surgery (AREA)
- Veterinary Medicine (AREA)
- Wood Science & Technology (AREA)
- Dental Tools And Instruments Or Auxiliary Dental Instruments (AREA)
- Application Of Or Painting With Fluid Materials (AREA)
- Adhesives Or Adhesive Processes (AREA)
- Compounds Of Alkaline-Earth Elements, Aluminum Or Rare-Earth Metals (AREA)
- Dental Preparations (AREA)
- Laminated Bodies (AREA)
- Paints Or Removers (AREA)
- Chemical Treatment Of Metals (AREA)
- Details Of Garments (AREA)
- Manufacturing Of Multi-Layer Textile Fabrics (AREA)
- Materials For Medical Uses (AREA)
- Confectionery (AREA)
Abstract
The adhesive strength of alumina articles to acrylic adhesive cements is enhanced by forming an essentially silica coating on the bonding surface of the article by the steps of coating said surface with an organosilicon compound such as a silane and then pyrolyzing the organosilicon coating to volatilize the organic components thereof to thereby leave an essentially silica coating.
Description
14"
I
i ~i* 600803 COMMONWEALTH OF AUSTRALIA PATENTS ACT 1952 Form COMPLETE SPECIFICATION FOR OFFICE USE Short Title: Int. Cl: Application Number: Lodged: Complete Specification-Lodged: Accepted: Lapsed: Published: Priority: 2C 17 U4-.~ci Related Art: TO BE COMPLETED BY APPLICANT Name of Applicant: Address of Applicant: Actual Inventor: JOHNSON JOHNSON DENTAL PRODUCTS 20 Lake Drive, East Windsor, NEW JERSEY,
U.S.A.
Albert C. Chen; Robert D. DeLuca; Robin M.
Forbes Jones; Donald S. Mueller and Mary S.
Yeganeh Address for Service: GRIFFITH HASSEL FRAZER 71 YORK STREET SYDNEY NSW 2000
AUSTRALIA
Complete Specification for the invention entitled: ADHESIVE PRIMER FOR ALUMINA ARTICLES The following statement is a full description of this invention, including the best method of performing it known to me/us:- 0538A:rk -il- This invention relates to the adhesive priming of alumina articles such as orthodontic brackets.
BACKGROUND OF THE INVENTION 15 Orthodontic brackets made of crystalline alumina (sapphire) tr S have been proposed. Such brackets are described in United States patent application Serial No. 743,851, filed on June 12.
1985, assigned to the same assignee as this application.
Orthodontic brackets are usually bonded directly to teeth with an acLylic cement. It has proven to be difficult to obtain sufficient bond strength between acrylic cements and crystalline alumina brackets to ensure that such brackets will not come off during normal use.
I One approach to improving the bond strength between c ~crystalline alumina orthodontic brackets and acrylic cements is described in U.S. Patent No. 4.595,598 and application Serial No. 806,712, the parent applications to this application. That approach was to form a thin, adherent coating of a siliceous material such as silica on the surface of the alumina. The silica coating increases the bond strength of the alumina to acrylic cements, especially when primed with a silane coupling agent. The specific methods for forming the siliceous coating on the alumina that are disclosed in the said parent JDC 155 t0 :1 15 1 20 I I -2applications include cathode sputtering, plasma deposition, and electron beam evaporation.
This invention provides an improved method for forming a thin, adherent coating of a siliceous material on the surface of alumina, preferably crystalline alumina, to thereby enhance the bond strength to acrylic adhesive cements.
The invention provides a method for applying an alumina orthodontic bracket to the the tooth of a patient, said alumina orthodontic bracket comprising a base member including an alumina tooth contacting surface and a body member extending from said base member, said body member including walls defining an archwire groove, which process comprises the steps of: coating said alumina tooth contacting surface with a thin adherent coating comprising silica; applying a silane coupling agent to said alumina tooth contacting surface having thereon a. thin adherent coating comprising silica; and bonding said bracket to the surface of a tooth with an acrylic cement, wherein said step comprises the steps of: coating said tooth contacting surface with an organosilicon compound; and subjecting the product of step to elevated temperature to pyrolyze the organic portion of said organosilicon compound to thereby produce an alumina orthodontic bracket having the alumina tooth contacting surface coated with a composition comprising silica.
JDC 155
L.-
-3.
RELEVANT ISSUED PATENTS Norling et al. in U.S. Patent No. 4,364,/3M. discloses the deposition of an oxide layer such as alumina or silica on a substrate to enhance the adhesive bonding of the substrate to polymers.
Acrylic orthodontic bracket cements are known, as is illustrated by Johnston, U.S. Patent No. 4,363,624, and by Orlowski et al., U.S. Patent No. 4,479,782.
A patei~t to Gobel et al., U.S. Patent No. 4,600,390, discloses the deposition by flame hydrolysis of a coating of a Gig* mixture of silica and carbon to a metallic dental przosthesis as an adhesion-promnoting layer. The filing date of Gobel et al., December 26, 1984. is later than the April 23. 1984, filing date of Applicants' parent application. Serial No. 602.874.
BRIEF DESCRIPTION OF THE DRAWINGS Fig. 1 is a schematic representation of apparatus for producing a crystalline alumina rod from which crystalline alumina orthodontic brackets can be machined; Fig. 2 is a top plan view of a die that is used in the apparatus of Fig. 1; Fig. 3 is a perspective view of a crystalline alumina rod produced by the apparatus of Fig. 1: Fig. 4 is a perspective view of the rod of Fig. 3 having an archwire groove machined therein; Fig. 5 is a perspective view of a series of bracket blanks cut from the rod of Fig. 4; Fig. 6 is a top plan view of the blanks of Fig. Fig. .7 is a perspective view of a crystalline alumina '~*~~/Aorthodontic bracket machined from the blanks of Fig. 6: i, -4- Fig. 8 is a top plan view of the bracket of Fig. 7; Fig. 9 is a view similar to Fig. 4, showing adhesion-promoting grooves cut in the bottom surface of the rod; Fig. 10 is a perspective view of a series of brackets machined from the rod of Fig. 9; Fig. 11 is a top plan view of the brackets of Fig. Fig. 12 is a perspective view, enlarged, of one of the brackets of Fig. 10; and Fig. 13 is a side view of the bracket of Fig. 12.
The major novelty of the invention resides in the step of coating the bonding surface of an alumina article with an S organosilicon compound, and then pyrolyzing the coating (in air or other oxidizing atmosphere) to volatilize the organic Smoieties in the coating to thereby leave a coating of a siliceous material that is predominantly silica. The organosilicon compounds that can be used for this purpose include the organosilane compounds such as those that are employed as coupling agents, silicate esters, and other organosilicon compounds. Specific illustrative examples include gamma-methacryloxypropyltrimethoxysilane, gamma-aminopropyltrimethoxysilane, vinyltriethoxysilane, allyltrimethoxylsilane, dimethyldiethoxysilane.
dihydroxydiphenylsilane. triethoxysilane, trimethoxysilane.
triethoxysilanol, 3-(2-aminoethylamino)propyltrimethoxysilane.
gamma-glycidoxypropyltrimethoxysilane. methyltrimethoxysilane.
JDC 155 vinyltriacetoxysilane. vinyl-tris(2-methoxyethoxy)silane, methyltriethoxysilane. tetraethyl orthosilicate, tetramethyl orthosilicate, and similar compounds.
The organosilicon compound is coated on the bonding surface by any convenient method. For instance, the alumina article can be immersed in an organic solvent solution of the organosilicon compound, removed from the solution, and (c) subjected to moderately elevated temperature to evaporate the solvent, thereby leaving a coating of the organosilicon compound on the entire surface of the article (including the bonding surface). Prior to the coating step, the article should be thoroughly cleaned and dried to enhance the adhesion of the organosilicon compound to the surface of the alumina.
After the solvent has been evaporated, the coated articles are subjected to a pyrolysis step in an oxidizing atmosphere such as air to volatilize the organic portion of the organosilicon compound, and to leave a coating that is essentially silica on the bonding surface of the alumina article. The specific conditions used in the pyrolysis step are not critical; the important factors are to use a temperature high enough to volatilize ("burn off") the organic moieties in the organosilicon compound, and to carry out the step for a period of time sufficient to volatilize essentially all of the organic moieties and to convert the silicon present to silica. Routine experimentation will suffice to determine the best conditions to use in particular cases.
The experimental section below describes specific embodiments of the invention wherein the alumina article is a crystalline alumina orthodontic bracket, and wherein the bonding surface the surface to be bonded to a substrate) is the tooth contacting surface of the bracket.
JDC 155 n j -6- General Procedures A. Cleaning Procedure Charge 100 mL of 45% aqueous KOH solution into a 200 mL beaker. Between 5 and 40 sapphire orthodontic brackets are added and stirred magnetically at 80 0 C for 1 hour. The brackets are collected on a sieve and washed with deionized water. The brackets are collected on a sieve again and stirred in 100 mL of 3% aqueous H3PO4 (in a 200 mL beaker) at for one hour. The brackets are collected on a sieve from the acid solution, washed in deionized water, and then stirred in 100 mL of deionized water at 80 0 C for 1 hour. The brackets are finally collected on a sieve again.
B. Heating Procedure I 4r o rr a. Sapphire brackets from the Cleaning Procedure step are heated in a furnace at 350°C for 16 hours. They are removed and stored immediately in a dessicator containing desiccants such as "drierite".
C. Heating Procedure II Same as above except the heating schedule is changed to 600°C for 1 hour.
D. Sapphire Brackets Two types of sapphire test specimens have been used: a. Brackets Sapphire orthodontic brackets which have wire slots and tie wings on the top side and a slight curvature at the base; and JDC 155 -7b. Chips Sapphire pieces having dimensions similar to that of brackets but have only flat surfaces on top and at the base.
Since the bond strengths of the two types are substantially equivalent, both will be referred to as "brackets".
E. Wire Mesh Substrate Onto the flat surface of a steel cylinder having a diameter of mm and a height of 20 mm is soldered a flat wire mesh mesh size), which is 6 mm x 6 mm in size. This substrate is used for bonding sapphire brackets. The wire mesh provides mechanical locking with the orthodontic adhesive. The substrate-sapphire assembly is then tested for bond strength on an Instron instrument.
This procedure is used to ensure that the bond strength measured is between the sapphire and the acrylic cement, and not between the cement and the steel cylinder substrate.
I F. Silane Solution S 25 Into 84 g of isopropyl alcohol in a 250-mL wide-mouth polyethylene bottle is added 2 g of gamma-methacryloxypropyltrimethoxysilane ("A-174 silane", from S Union Carbide), 6 g of deionized water, and 8 g of glacial acetic acid. After closing the bottle, the contents are mixed by swirling, and the bottle is placed in a water bath at 37°C.
The silane solution can be used between 2 and 23 hours after preparation.
JDC 155 r .7 -8- G. Single Priming Process Brackete which have gone through the Cleaning PrOcedure and Heating Procedure I (or Heating Procedure II) are removed from the desiccator and added to a beaker containing the Silane Solution (about 1-2 ml solution per bracket). After 10 minutes the brackets are collected on a sieve and transferred to an aluminum drying dish. The dish is then stored in a desiccator (no desiccant) for 30 min. The primed brackets are i subsequently heated in a forced draft oven at 110 0 C for 1 hour to volatilize the solvent and to cure the silane, as is I f i conventional in the art. The brackets are then stored in a S desiccator.
H. Pyrolysis Step Brackets that have been Single Primed are heated according to Heating Procedure I or Heating Procedure II. Heating Procedure I or II (both done in air), when carried out on primed brackets, effectively pyroly:es all the organic portion of the silane, leaving a coating that is essentially silica. The brackets having the essentially silica coating may then be i Isubjected to a second prining with A-174 silane ("Double i 25 Priming"). The second primer layer is then used in the conventional manner as a coupling '.gent.
SBond Strength Testing The two pastes of a chemical-cured orthodontic adhesive (e.g.
"Achieve" marketed by Johnson Johnson Dental Products Company or "Concise" marketed by 3M) are mixed and a small amount is applied to the base of a primed sapphire bracket, which is then pressed against the Wire Mesh Substrate for 1 min. The bonded pairs are stored in water at 37°C for 16 hours. An Instron JDC 155 -9instrument is used to measure the shear strength of the bonds at a crosshead speed of 0.5 mm per min.
The acrylic adhesive used in these experiments was "Achieve", an acrylic cement containing bis-GMA. bisphenol A dimethacrylate, triethylene glycol dimethacrylate, and silica fillers.
0 The shear strength test was carried out on an Instron tester as !follows: The Wire Mesh Substrate to which is bonded the sapphire Sbracket is clamped securely in the Instron tester. A rod from the Instron is brought to bear against the side of the bracket at a rate of 0.5 mm per minute until the bracket breaks away from the wire mesh. The force required to break the bracket away from the wire mesh is then recorded as MPa (1 MPa=145 psi).
S 20 Experimental Results j Example 1 (Control) Twelve sapphire brackets, unprimed, went through the Cleaning Procedure, Heating Procedure I, and Bond Strength Testing steps. The average shear strength obtained was 3.6 MPa (std.
dev. 2.6 MPa).
Example 2 (Control) Twenty two sapphire brackets were treated according to the Cleaning procedure and Heating Procedure I and were then primed with A-174 silane in the conventional manner. During the Single Priming, half of the brackets (Group A) were dried and heated (at 110°C for 1 hour) with the bases facing up while the JDC 155
P
other half (Group B) with the bases facing down. Bond Strength Testing showed that Group A had shear strengths of 12.3 MPa (Std. dev. 7.7 MPa) and Group B had shear strengths of 16.7 MPa (Std. dev. 5.3 MPa).
Example 3 (Control) Identical to Example 2, except the heating step (prior to priming) was changed to Heating Procedure II (600 0 C/1 hr). The average shear strengths were: Group A, 8.8 MPa (Std. dev. 5.1 MPa), and Group B. 17.8 MPa .(Std. dev. 6.5 MPa).
o tq
CO
r i d i j 1
E
i Example 4 Twenty sapphire brackets went through the Cleaning Procedure and Heating Procedure I (350 0 C/16 hrs) steps and were then Single Primed. Double Priming was then carried out after first pyrolyzing the coating of cured silane by heating the single primed brackets at 350 0 C/16 hrs in air. Shear strength tests showed that Group A (bases faced up) had bond strengths of 25.7 MPa (Std. dev. 6.9 MPa), and Group B (bases faced down) had bond strengths of 24.9 MPa (Std. dev. 11.3 MPa).
Examples 5-7 Triplicate experiments were carried out using the Heating Procedure II (600 0 C/1 hr) to pyrolyze the first coating of cured .silane followed by Double Priming. The shear bond strengths are shown below.
Group A (Bases Up) Group B (Bases Down) Ave. Std. Dev. Ave. Std. Dev.
Example 5. MPa Example 6, MPa Example 7. MPa 36.0 29.6 28.2 8.2 6.9 8.6 30.1 31.7 30.8 7.1 10.6 7.6 JDC 155 -11- Example 8 (Control) Eighteen sapphire brackets underwent Single Priming and were then thermocycled in water between 0 0 C/30 sec. and 60°C/30 sec. After 700 cycles the average shear bond strength was 11.6 MPa (Std. dev. 5.8 MPa). The average bond strength after being kept in water at 37 0 C for 16 hours was 18.6 MPa (Std. dev. 4.3 MPa).
Example 9 Twenty-two sapphire brackets which went through the Double Priming procedure, with Heating Procedure II (in air) between the two priming steps, were bonded to the Wire Mesh Substrates and were thermocycled between 0°C/30 sec and 60 0 C/30 sec.
After 1,000 cycles, the average shear bond strength remained virtually unchanged at 35.7 MPa (Std. dev. 11.3 MPa).
Example 10 (Control) Quartz (silica) pieces having dimensions similar to those of sapphire brackets went through the Cleaning Procedure, Heating Procedure II, Single Priming, and Bond Strength Testing steps.
The results are as follows: Group A (bases faced up) 19.6 MPa (Std. dev. 9.4 MPa), and Group B (bases faced down) 21.4 MPa (Std. dev. 4.5 MPa).
Example 1l-(Control) The bases of sapphire brackets were sputtered coated with silicon dioxide. Twenty four such brackets were single primed and the bond strengths determined. The results show that Group A (bases faced up) had shear strengths of 26.1 MPa (Std. dev.
9.0 MPa), and Group B (bases faced down) had shear strengths of JDC 155
LJ
-t -12- 22.2 MPa (Std. dev. 7.5 MPa).
Example 12 Four round sapphire disks, 6 mm in diameter, and 2 mm thick.
were treated as follows, in the sequence shown: Heating Single Heating Double I Priming II Priming Sample Cleaning Yas Yes Yes Yes Yes Yes Yes Yes No Yes Yes Yes No No Yes Yes No No No Yes or tr 151 The samples were analyzed by ESCA (Electron Spectroscopy for Chemical Analysis) at 285 electron volts.
The results show that on the surface of the sapphire, the ratios of silicon atoms (from the primer) to aluminum atoms (from the sapphire) are as follows: Sample 1 Si/Al 0.000 0.0460 0.1966 0.2376 This invention is employed in connection with alumina articles, preferably crystalline alumina articles, and more preferably crystalline alpha-alumina.
As used herein, the term "crystalline alumina" is intended to include only essentially monocrystalline alumina,-that is.
JDC 155 4 -13alumina comprised of a single crystal or two or more single crystals grown together longitudinally but separated by a relatively small angle (usually within 40, determined with respect to the C-axes of neighboring single crystals) grain boundary.
In a preferred aspect of the invention, the alumina article is a crystalline alumina orthodontic bracket made entirely from crystalline alpha-alumina. Such a bracket can be produced by first drawing a crystalline alpha-alumina rod from a melt, wherein the rod has a predetermined cross-sectional configuration, by slicing the rod into individual blanks, and .I then machining the blanks to produce the bracket. As will be made apparent by the discussion below, the cross-sectional '15 configuration of the rod is approximately the configuration of the cross-section of an orthodontic bracket taken in a plane I that is perpendicular to the top and bottom faces of the bracket and is approximately parallel to the two side faces of the bracket. (By "approximately parallel" is meant not more than about 12° from parallel, for reasons that will be made clear below.) The terms "top and bottom faces" and "side faces" refer to the top, bottom, and side surfaces, respectively, of the bracket when looking directly at the front of the bracket (the "front of the bracket" is the surface opposite the tooth contacting surface) in the position the bracket would assume when installed on a tooth with the patient in the upright position. In the embodiments illustrated herein, the brackets have two pairs of tie wings, and the said plane is taken through a pair of tie wings. Thus, the said predetermined cross-sectional configuration will preferably include two pairs of tie wings and a base.
The preferred procedure for producing a crystalline alpha-alumina rod having a predetermined cross-sectional configuration is the EFG (for Edge-defined. Film-fed, Growth) JDC 155 1:~ -14modification of the Czochralski process for growing crystalline alpha-alumina. The EFG process is described by LaBelle in "EFG The Invention and Application to Sapphire Growth", in Journal of Crystal Growth. 50. pages 8-17 (September 1980). See also LaBelle. U. S. Patent Nos. 3,591.348. and 3.870.477, LaBelle et al.. U. S. Patent Nos. 3,701.636 and 3.915.662.
and other patents and articles cited in the Journal of Crystal Growth article.
Fig. 1 is a schematic representation of apparatus for producing a crystalline alpha-alumina rod having a predetermined cross-sectional configuration by the EFG process. The apparatus 20 includes a crucible 22 15 containing molten alumina 24. A die 26 made of a suitable material such as molybdenum or iridium is positioned such that the bottom of the die 26 is immersed in the molten alumina 24, and the top of the die 26 is above the surface of the melt 24. A vertical distance from the top of the melt 24 to the top surface 28 of the die 26 of up to 2 Imillimeters is permissible. (This distance is exaggerated in Fig. 1 for clarity.) Fig. 2 shows the top surface 28 of the die 26. The top surface 28 is smooth, flat, and has the overall approximate shape of the desired configuration of the cross-section of the crystalline alpha-alumina rod (shown in Fig. 3) from which the brackets are made, including the configuration of a pair of tie wings, shown as 29 and 31, and the base of the bracket, shown as 33.
It is important that the sides 32 and the top surface 28 of the die 26 meet in a sharp 90° angle, in order to minimize imperfections in the surface of the growing rod The die 26 contains a capillary passage 34 through which molten alumina 24 is drawn. The melt 24 is drawn JDC 155
I
from the crucible 22 through the capillary 34 to the top surface 28 of the die 26, where it spreads out and completely covers the said top surface 28 with a film of j| molten alumina. However, because molten alumina and molybdenum or iridium have the appropriate wettability relationship, the molten alumina film stops at the edge of the surface 28. Therefore, crystalline alpha-alumina crystal grown or pulled from this film of molten alumina assumes a cross-sectional configuration substantially exactly the same as the configuration of the top surface 28 of the die 26. Thus, the rod 30 (which had been Sstarted by a seed crystal, as in the Czochralski process) pulled by a pulling mechanism 36 from the film of molten alumina on the top surface 28 of the die 26 will have a cross-sectional configuration substantially identical to !j the configuration of the top surface 28 of the die 26. It (I has been found to be convenient to grow the rod 30 to a length of about two inches (about 5 centimeters) in order to minimize any machining problems that could be caused by the failure of the rod to grow exactly straight.
i The crystal orientation of the growing rod may prove to be Jii important (at least economically, and perhaps also from a performance standpoint) in the practice of the invention.
In the case of crystalline alpha-alumina, the crystal orientation can be defined with reference to the C axis of the crystal. (The C axis is perpendicular to the plane which contains the simplest arrangement of atoms in the crystal unit cell. Stated another way. the C axis is perpendicular to the plane which contains the a and a 2 axes.) The minimum amount of strain developed in the growing crystal will occur if the C axis is found in a plane perpendicular to the longitudinal axis L of the rod (See Fig. This has proven to be the optimum crystal orientation in some cases. (As is known, in the JDC 155 S1 -16art. the growing cristal will assume the crystal orientation of the seed crystal.) Regardless of the crystal orientation of the rod 30, it is preferred to anneal the rod 30 prior to machining so as to relieve stresses in the crystal to minimize the chances of breakage during machining. A typical annealing cycle would be to heat the rod 30 from room temperature up to 1950-2000 C at an even rate for about two hours, to maintain the rod 30 at 1950-2000 0 C for 4 to 6 hours, and to then cool the rod 30 down to room temperature at an even rate for two hours. The entire annealing cycle is preferably carried out under an inert atmosphere such as o %argon.
t The archwire groove may be ground in the rod to produce r the grooved rod 86 shown in Fig. 4. In Figs. 4-8 and 10-11, the archwire groove is defined by walls 88a, 88b, ,88c.) The bracket blanks 92 that are cut from the rod 86 are cut at a slight angle, as is seen in Figs. 5 and 6. Thus, instead of making the cuts in the rod 86 in a plane normal or perpendicular to the longitudinal axis L of the rod, tthe cuts are made in the following manner: Holding the rod 86 in position withl the longitudinal axis L in a horizontal plane and the face having the longitudinal groove on top, each cut is made in a vertical plane that is angled slightly up to about 120) at an angle a from the vertical plane that is perpendicular to the longitudinal axis L of the rod 86. This is best seen in Fig. 6.
The "saddles" (defined by walls 140, 142. 144 see Fig.
12) and the two base concavities (shown as 73 and 74 in JDC 155 B2 -17o st 0 1 011 o 1 O 1 01 C *1 t C.1
I
Fig. 7) can be machined in the bracket prior to cutting the individual brackets from the rod 86. This is preferred because it is easier to handle the rod 86 than the individual bracket blanks 92. The machining of the saddles can then be done with a diamond grinding wheel by feeding the rod stepwise to the wheel and cutting a series of grooves across the rod, wherein the said grooves will be oriented generally perpendicularly to the longitudinal axis L of the rod 86 (although, when rhomboidally shaped brackets are being produced, the cut will depart from the perpendicular by the angle, a, as discussed above), and the two base concavities can be ground in a similar stepwise manner with a double-contoured diamond grinding wheel whose grinding edge is rounded or radiused to the 15 appropriate degree so that the two concavities can be ground at the same time. Figs. 10 and 11 show the saddles and both concavities already machined in the brackets 150 as the rod is cut into individual brackets.
After machining, the brackets are preferably annealed under the conditions disclosed above for drawn rods.
Then, the brackets may be polished to smooth off contours and to remove any surface imperfections which could encourage propagation of cracks. If a polishing step is employed, a flux polishing procedure would be recommended in which the flux is partially saturated with alumina so that the removal of alumina from the surface of the bracket will proceed at a controllable rate. One preferred flux is composed of 51.2 per cent LiBO 2 12.8 per cent Li B 0 16 per cent Al 0 3 and 20 per 2 4 V 2 cent LiF (the percentages are by weight). The machined brackets are immersed in molten flux at 8500 to 900 0
C.
for a few minutes, from about four to about thirty minutes, and then removed. After cooling, the brackets can be immersed in aqueous hydrofluoric acid to remove any JDC 155 -18flux adhering to the surfaces of the brackets. Experience has demonstrated that the polishing step may be omitted.
and in fact it may be undesired in many cases because of the problems it causes in holding to the dimensional specifications, especially in the archwire grooves.
Other processes for polishing the surface of crystalline alpha-alumina objects are known, and may be used if desired. Such other processes are disclosed, for example, by Noble, in U. S. Patent No. 4,339,300, and Manasevit, in U. S. Patent No. 3,546,036.
A means of enhancing the mechanical adhesion of the bracket to the surface of the tooth is shown in Figs.
15 9-13. Small grooves 120 may be cut in the bottom surface of the rod 122, as is shown in Fig. 23. The grooves 120 extend the entire length of the rod 122. Typically, the grooves 120 will be from about 6 to 15 mils wide, with a depth about one and one-half times the width. The grooves 120 are preferably angled slightly (about 12-15° from a direction that is generally perpendicular to the tooth contacting surface of the bracket 150. as is seen most clearly in Fig. 13). The grooves 120 will extend in a direction that is generally parallel to the orientation of the archwire groove. That is, the grooves 120 will be generally parallel to the walls 88a, 88b. 88c that define the archwire groove.
While the invention has been described most particularly in terms of bonding crystalline alumina orthodontic brackets to the surface of teeth with acrylic adhesive cements, it is applicable to the bonding of any crystalline alumina article to any substrate using an acrylic cement. Such other alumina articles include ceramic polycrystalline alumina orthodontic brackets such JDC 155 120 7 -19as those described by Reynolds in U.S. Patent Nos.
4,216.583 and 4,322.206 and Walishein in U.S. Patent No.
4,*219,*617.
JDC 155
Claims (7)
1. A method for applying an alumina orthodontic bracket to the the tooth of a patient, said alumina orthodontic bracket comprising a base member including an alumina tooth contacting surface and a body member extending from said base member, said body member including walls defining an archwire i ',10 groove, which process comprises the steps of: i coating said alumina tooth contacting surface I with a thin adherent coating comprising silica; 15 applying a silane coupling agent to said alumina tooth contacting surface having thereon a thin adherent coating comprising silica; and i bonding said bracket to the surface of a tooth with an acrylic cement, i wherein said step comprises the steps of: coating said tooth contacting surface with an organosilicon compound; and subjecting the product of step to elevated temperature to pyrolyze the organic portion of said organosilicon compound to thereby produce an alumina orthodontic bracket having the alumina tooth contacting surface coated with a composition comprising silica.
2. The method of claim 1 wherein the silane is gamma-methacryloxypropyltrimethoxysilane. 7907S/SL :I I L- r; t 21
3. The method of claim 2 wherein the silane is gamma-methacryloxypropyltrimethoxysilane.
4. The method of claim 1 wherein the alumina bracket is a crystalline alumina bracket.
The method of claim 4 wherein the organosilicon compound is a silane.
6. The method of claim 5 wherein the silane is gamma-methacryloxypropyltrimethoxysilane.
7. A method for applying an alumina orthodontic bracket substantially as herein described but excluding prior art and control methods. DATED this 25th day of May 1990 1 JOHNSON JOHNSON DENTAL PRODUCTS By Their Patent Attorney GRIFFITH HACK CO. 7907S/SLV
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US2543887A | 1987-03-13 | 1987-03-13 | |
| US025438 | 1987-03-13 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| AU1305888A AU1305888A (en) | 1988-09-15 |
| AU600803B2 true AU600803B2 (en) | 1990-08-23 |
| AU600803C AU600803C (en) | 1993-12-23 |
Family
ID=
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4595598A (en) * | 1984-04-23 | 1986-06-17 | Johnson & Johnson Dental Products Company | Crystalline alumina composites |
| US4639218A (en) * | 1984-04-23 | 1987-01-27 | Johnson & Johnson Dental Products Company | Crystalline alumina orthodontic bracket |
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4595598A (en) * | 1984-04-23 | 1986-06-17 | Johnson & Johnson Dental Products Company | Crystalline alumina composites |
| US4639218A (en) * | 1984-04-23 | 1987-01-27 | Johnson & Johnson Dental Products Company | Crystalline alumina orthodontic bracket |
| AU580296B2 (en) * | 1984-04-23 | 1989-01-12 | Johnson & Johnson Dental Products Co. | Adhesively bonded crystalline alumina articles |
Also Published As
| Publication number | Publication date |
|---|---|
| PT86945B (en) | 1995-03-01 |
| NO881112D0 (en) | 1988-03-11 |
| IE62251B1 (en) | 1995-01-11 |
| PH25562A (en) | 1991-08-08 |
| GR1000078B (en) | 1990-11-29 |
| DE3873381T2 (en) | 1992-12-10 |
| GR880100150A (en) | 1989-01-31 |
| IE880731L (en) | 1988-09-13 |
| DE3873381D1 (en) | 1992-09-10 |
| KR880010740A (en) | 1988-10-24 |
| JP2563122B2 (en) | 1996-12-11 |
| DK170816B1 (en) | 1996-01-29 |
| EP0282325A3 (en) | 1990-03-07 |
| FI90972C (en) | 1994-04-25 |
| FI881161L (en) | 1988-09-14 |
| DK134488A (en) | 1988-09-14 |
| AU1305888A (en) | 1988-09-15 |
| FI881161A0 (en) | 1988-03-11 |
| NO881112L (en) | 1988-09-14 |
| NZ223704A (en) | 1990-02-26 |
| ATE79112T1 (en) | 1992-08-15 |
| PT86945A (en) | 1989-03-30 |
| ZA881773B (en) | 1989-11-29 |
| CA1298743C (en) | 1992-04-14 |
| BR8801116A (en) | 1988-10-18 |
| EP0282325B1 (en) | 1992-08-05 |
| ES2034195T3 (en) | 1993-04-01 |
| DK134488D0 (en) | 1988-03-11 |
| EP0282325A2 (en) | 1988-09-14 |
| FI90972B (en) | 1994-01-14 |
| KR970006636B1 (en) | 1997-04-29 |
| MY103232A (en) | 1993-05-29 |
| JPS63278582A (en) | 1988-11-16 |
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